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PALAPA C2

NORAD 23864 Payload GEO 1996-030A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36125 km
Apogee
36168 km
Inclination
11.6°
Period
1454.5 min
Mean Motion
0.99000497 rev/day
TLE Epoch
2026-05-08 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,147 km
Orbital Velocity11,023 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0005
Semi-Major Axis42,518 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Indonesia
Launch Date
1996-05-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1996-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
PALAPA C2 is an active satellite operated by Indonesia, launched on 1996-05-16 from Guiana Space Centre, Kourou. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,125 km and 36,168 km with an inclination of 11.6°. It travels at approximately 11,023 km/h (3.06 km/s), completing one full orbit every 24.2 hours — that’s roughly 0.99 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks PALAPA C2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PALAPA C2 occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 11.6°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
PALAPA C2 orbits at approximately 36,147 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,023 km/h — it just keeps pace with the ground below. With an inclination of 11.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
PALAPA C2 is operated by Indonesia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23864. You can track PALAPA C2 in real time on Orbital Radar’s live tracker.
PALAPA C2 was launched on 1996-05-16 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions.
Yes — Orbital Radar tracks PALAPA C2 (NORAD ID 23864) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time.
PALAPA C2 travels at approximately 11,023 km/h (6,849 mph) — roughly 3.06 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
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